| 发明名称 | Method for setting a gear ratio of a fan drive gear system of a gas turbine engine | ||
| 摘要 | A gas turbine engine includes a fan section including a fan rotatable about an axis. A speed reduction device is connected to the fan. The speed reduction device includes a planetary fan drive gear system with a planet gear ratio of at least 2.5. A bypass ratio is greater than about 11.0. | ||
| 申请公布号 | US8814494(B1) | 申请公布日期 | 2014.08.26 |
| 申请号 | US201414203863 | 申请日期 | 2014.03.11 |
| 申请人 | United Technologies Corporation | 发明人 | Sheridan William G.;Hasel Karl L. |
| 分类号 | F01D1/24;F02C7/36 | 主分类号 | F01D1/24 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. A gas turbine engine comprising: a fan section including a fan rotatable about an axis; and a speed reduction device connected to the fan, wherein the speed reduction device includes a planetary fan drive gear system with a planet gear ratio of at least 2.5, wherein a bypass ratio is greater than about 11.0. | ||
| 地址 | Hartford CT US | ||